论文标题
太阳能X射线监视器的地面校准板上Chandrayaan-2轨道器
Ground Calibration of Solar X-ray Monitor On-board Chandrayaan-2 Orbiter
论文作者
论文摘要
Chandrayaan-2是印度第二个月球任务,它带有一个名为Solar X射线监视器(XSM)的光谱仪,以执行太阳的软X射线光谱测量值,而伴侣有效载荷测量来自月球的荧光发射。这两个有效载荷一起将提供对月面上元素丰度的定量估计。 XSM还有望为太阳X射线研究提供重要的贡献,其时间最高和能量分辨率测量值。为此,XSM采用了硅漂移检测器,并在1-15 keV范围内对入射光子进行能量测量,分辨率在5.9 keV时的分辨率小于180 eV,这是在广泛的太阳能X射线强度上。使用实验室X射线源以及X射线光束线设备,已使用XSM进行了广泛的接地校准实验,以确定定量光谱分析所需的仪器响应矩阵参数。这包括在各种观察条件下的增益,光谱重新分布函数和有效区域的测量。还研究了XSM在高入射通量以及死亡时间和堆积特性下保持光谱性能的能力。本文提供了XSM有效载荷的这些接地校准实验的结果。
Chandrayaan-2, the second Indian mission to the Moon, carries a spectrometer called the Solar X-ray Monitor (XSM) to perform soft X-ray spectral measurements of the Sun while a companion payload measures the fluorescence emission from the Moon. Together these two payloads will provide quantitative estimates of elemental abundances on the lunar surface. XSM is also expected to provide significant contributions to the solar X-ray studies with its highest time cadence and energy resolution spectral measurements. For this purpose, the XSM employs a Silicon Drift Detector and carries out energy measurements of incident photons in the 1 -- 15 keV range with a resolution of less than 180 eV at 5.9 keV, over a wide range of solar X-ray intensities. Extensive ground calibration experiments have been carried out with the XSM using laboratory X-ray sources as well as X-ray beam-line facilities to determine the instrument response matrix parameters required for quantitative spectral analysis. This includes measurements of gain, spectral redistribution function, and effective area, under various observing conditions. The capability of the XSM to maintain its spectral performance at high incident flux as well as the dead-time and pile-up characteristics have also been investigated. The results of these ground calibration experiments of the XSM payload are presented in this article.